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Introduction to Acoustics

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590 Part E Music, Speech, Electroacoustics<br />

Part E 15.2<br />

Skele<strong>to</strong>n Curves<br />

In this idealised model, the normal modes of the structure<br />

at high frequencies will be similar <strong>to</strong> those of the<br />

individual plates. Such modes will only be significantly<br />

perturbed when the resonances of the separate plates are<br />

close <strong>to</strong>gether, apart from a general background interaction<br />

from the average weak but cumulative interaction<br />

with all other distant modes. Woodhouse [15.76]hasrecently<br />

shown that the averaged amplitude and phase of<br />

the admittance can be described by skele<strong>to</strong>n curves, indicated<br />

by the dashed lines in Fig. 15.58, on which peaks<br />

and troughs of height Q and 1/Q and phase changes<br />

from individual resonances are superimposed. These<br />

curves were evaluated analytically for the rotational admittance<br />

across the two feet of a bridge mounted on the<br />

front plate of an idealised rectangular box-like violin<br />

without f-holes but with a soundpost close <strong>to</strong> the treble<br />

foot of the bridge.<br />

At low frequencies the averaged input impedance<br />

across the two feet of the bridge is largely reactive, with<br />

a value close <strong>to</strong> the static springiness, which can be identified<br />

with the low-frequency limit of the normal-mode<br />

admittance �<br />

n iω/mnω 2 n<br />

, where the effective mass of<br />

each mode will depend on where and how the instrument<br />

is excited. However, at high frequencies the admittance<br />

becomes largely resistive resulting from internal damping<br />

and energy loss <strong>to</strong> the closely overlapping modes.<br />

The use of skele<strong>to</strong>n curves enables Woodhouse <strong>to</strong> illustrate<br />

the effect of various different bridge designs on<br />

the overall frequency response of a violin, without having<br />

<strong>to</strong> consider the exact positions, spacing or damping<br />

of the individual resonances of the shell structure. Although<br />

the idealised model is clearly over-simplistic, the<br />

general trends predicted by such a model will clearly be<br />

relevant <strong>to</strong> any multi-resonant shell model.<br />

Soundpost and f-Holes<br />

The soundpost and f-holes cut in<strong>to</strong> the front plate of the<br />

violin and related instruments have a profound effect on<br />

the frequencies and waveforms of the normal modes,<br />

illustrated schematically by the right-hand set of examples<br />

in Fig. 15.57. The f-holes create an island area on<br />

which the bridge sits, which separates the <strong>to</strong>p and lower<br />

areas of the front plate. Like the rose-hole on a guitar illustrated<br />

in Fig. 15.56, the additional internal free edges<br />

introduced by the f-holes tend <strong>to</strong> localise the vibrations<br />

of the front plate <strong>to</strong> the regions above and below the island<br />

area. In addition, the soundpost acts as a rather rigid<br />

spring locking the vibrations of the <strong>to</strong>p and back plates<br />

<strong>to</strong>gether at it its ends. At low frequencies, the soundpost<br />

introduces an approximate node of vibration on both the<br />

<strong>to</strong>p and back plates, unless the frequencies of the uncoupled<br />

front and back plates modes are close <strong>to</strong>gether.<br />

For some low-frequency modes, the soundpost and<br />

f-hole have a relatively small effect on the modes of the<br />

shell structure, such as the twisting mode (a) and mode<br />

(c), when the plates vibrate in the same direction. However,<br />

the breathing mode (c) will be strongly affected by<br />

the soundpost forcing the front and back plates <strong>to</strong> move<br />

<strong>to</strong>gether across its ends.<br />

As indicated earlier, any string motion parallel <strong>to</strong><br />

the plates will exert a couple on the <strong>to</strong>p of the bridge. In<br />

the absence of the soundpost, only asymmetric modes<br />

of the <strong>to</strong>p plate could then be excited. However, <strong>to</strong><br />

satisfy the boundary conditions at the soundpost position,<br />

the rocking action now induces a combination of<br />

symmetric and antisymmetric plate modes (illustrated<br />

schematically in Fig. 15.57b), approximately doubling<br />

the number of modes that can contribute <strong>to</strong> the sound<br />

of an instrument including the very important lowerfrequency<br />

symmetric breathing modes. Because of the<br />

f-holes, the central island can vibrate in the opposite direction<br />

<strong>to</strong> the wings on the outer edges of the instrument.<br />

The mixing of symmetric and antisymmetric modes is<br />

strongly dependent on the position of the soundpost relative<br />

<strong>to</strong> the nodes of the coupled waveforms. As a result,<br />

the sound of a violin instrument is very sensitive <strong>to</strong> the<br />

exact placing of the soundpost. The difference in the<br />

sound of a violin with the soundpost first in place and<br />

then removed is illustrated in .<br />

To a good approximation, in the audible frequency<br />

range, the violin soundpost can be considered as a rigid<br />

body, as its first longitudinal resonance is ≈100 kHz,<br />

though lower-frequency bending modes can also be excited,<br />

particularly if the upper and lower faces of the<br />

soundpost fail <strong>to</strong> make a flat contact with the <strong>to</strong>p and<br />

back plates (Fang and Rogers [15.95]). At high frequencies,<br />

there is relatively little induced motion of the outer<br />

edges of <strong>to</strong>p and back plates, so that the impedance Z(ω)<br />

(force/induced velocity) measured at the soundpost position<br />

is simply given by the sum of the impedances at<br />

the soundpost position, Z(ω)<strong>to</strong>p + Z(ω)back, of the individual<br />

plates with fixed outer edges. If one knows the<br />

waveforms of the individual coupled modes, it is relatively<br />

straightforward <strong>to</strong> evaluate the admittance at any<br />

other point on the two surfaces, and hence <strong>to</strong> evaluate the<br />

rotational admittance across the two feet of the bridge<br />

(Woodhouse [15.76]).<br />

We have already described the important role of the<br />

bridge dynamics in the coupling between the strings and<br />

the vibrational modes of the instrument. For instruments<br />

of the violin family, the island region between the f-holes

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